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Year
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1976
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ABLATIVE MATERIALS
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AERODYNAMIC CONFIGURATIONS
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COST EFFECTIVENESS
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Combs, H. G.
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DESIGN ANALYSIS
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HEAT SINKS
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nasa technical reports server (ntrs)
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English
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Four hypersonic research airplane configurations found to be the most cost effective were selected for further refinement. The selection was based on a systematic analysis and evaluation of realistic designs, involving nine different configurations, evolving from three different structural/thermal concepts, coupled with existing rocket and sustainer engines. All configurations were constrained by the mission profiles, research requirements, aerodynamic envelope and maximum launch weight...
Topics: NASA Technical Reports Server (NTRS), AERODYNAMIC CONFIGURATIONS, HEAT SINKS, HYPERSONIC FLIGHT,...